GAOFEN 12 04, 57654
Orbit data source: Space-Track
GAOFEN 12 04, 57654 is a payload satellite owned by PLA SSF (CN) in SSO that was launched on Sun, 20 Aug 2023 UTC via a CHANG ZHENG 4C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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57654 intel report (Beta)
GAOFEN 12 04 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | SAST |
| Mission | Operational Defense Radar Imaging |
| Bus & Motor | CS-L3000B?, Unknown motor |
| Mass | ~3,000 kg wet, ~3,000 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 3 Pan, 8 m |
| Radar Cross Section | 10.846 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 GAOFEN 12 04
1 57654U 23123A 24356.14790035 .00002620 00000-0 34748-3 0 9996
2 57654 97.9111 271.0100 0004775 85.6782 274.4976 14.80677358 72295Epoch: 2024-12-21T03:32Z
Definitive object data (Epoch: 2024-12-21T03:32:58.59Z)
| Latitude | 0.00001° |
| Longitude | 127.56265° |
| Altitude | 629.948 km |
| Speed | 7.544 km/s |
| True Right ascension | 18h 04m 02s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 69.31045° |
| Longitude | 106.44265° |
| Altitude | 635.915 km |
| Speed | 7.548 km/s |
| Apparent Right ascension | 21h 08m 44s |
| Apparent Declination | 25° 01' 15" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:00:20 |
| Azimuth | 26.831° NE |
| Elevation | -20.05° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 627.571 km |
| Perigee altitude | 620.884 km |
| Semi-major axis | 7,002.364 km |
| Eccentricity | 0.0004775 |
| Inclination | 97.9111° |
| RAAN | 271.01° |
| Arg. of periapsis | 85.6782° |
| True anomaly | 274.44305° |
| Mean anomaly | 274.4976° |
| Eccentric anomaly | 274.47032° |
| Mean motion | 3.70404 °/min |
| BSTAR | 0.00034748 |
| Orbital period | 97.19 mins |
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Other satellites on launch #123 in the year 2023 (2023-08-20 UTC)
| GAOFEN 12 04, 57654 |
| CZ-4C R/B, 57655 |
GAOFEN 12 04 Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-21 18:16:36.755Z | 149.034° SSE | 2024-12-21 18:19:36.755Z | 91.586° ESE | 39.661° | 2024-12-21 18:23:36.755Z | 357.444° N |
| 7 mins | 2024-12-22 07:41:36.755Z | 2.249° NNE | 2024-12-22 07:44:36.755Z | 298.061° NW | 41.225° | 2024-12-22 07:48:36.755Z | 206.549° SW |
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